STC ST00055SE

Supplemental type certificate · LifePort LLC

Holder
LifePort LLC · United States
Status
Current · Reissued
Status date
May 10, 2019
Applied
August 9, 1993
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 25
Data sheet
TCDSA21EA

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of emergency medical stretcher, oxygen, and electrical systems.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Number ST00055SE

This certificate, issued to LifePort, LLC 1610 Heritage Street Woodland, WA 98674

Part 25* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet A21EA.

Original ProductType Certificate Number: A21EA Make: Canadair Model: CL-600-1A11, CL-600-2A12, and CL-600-2B16 Description of the Type Design Change: Installation of a patient loading and utility system (PLUS) in accordance with LifePort Master Drawing List No. 520-6000, Revision B, dated January 27, 1994, or later FAA approved revision is required as part of this installation.

NOTE: This installation includes provisions for mounting equipment in the cabin interior (via equipment sleds and arches). Equipment mounted on these provisions, which is not specified in the above drawing package, requires separate FAA approval.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of these model series on which other previously approved modification are incorporated unless the installer determines that the relationship between this change and any other previously incorporated approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, FAA approved Flight Manual Supplement (FMS) No. 29, dated January 28, 1994, or later FAA approved revision, must be included in the permanent records of the modified aircraft.

If the holder agree to permit another person to use this certificate to alter the product, the holder sha ll give the other person written evidence of that permission.

Date of application: August 9, 1993 Date reissued: January 25, 2007; May 10, 2019 Date of issuance: January 28, 1994 Date amended:

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Acting Manager, Seattle ACO Branch (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of Transferee)

(Address of Transferee)

(Number and Street)

(City, State, and ZIP Code)

from (Name of Grantor) (Print or Type)

(Address of Grantor)

(Number and Street)

(City, State, and ZIP Code)

Signature of Grantor (In Ink):

U.S. GPO: 1987-763-289

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 5

MakeModelData sheet
Bombardier Inc.CL-600-1A11 (CL-600)A21EA
Bombardier Inc.CL-600-2A12 (CL-601)A21EA
Bombardier Inc.CL-600-2B16 (CL-601-3A)A21EA
Bombardier Inc.CL-600-2B16 (CL-601-3R)A21EA
Bombardier Inc.CL-600-2B16 (CL-604)A21EA

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
May 10, 2019Reissued, currentCertificate
January 28, 1994Issued, earlier issueCertificate